Direct solution of the problem of optimizing control spatial motion of light aircraft in flight testing

Aviation technics and technology


Аuthors

Baranov V. N.*, Zaw L. O.**

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: vnb36@mail.ru
**e-mail: zaw.lin@mail.ru

Abstract

In this paper we solve the problem of synthesis of control algorithm light aircraft during flight

Keywords:

control algorithm, the dynamic equations, the functional synthesis of optimal control.


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